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Circuit topology and energy management method of satellite power source system

A technology of satellite power supply and circuit, which is applied in the field of satellite power supply system, can solve the problems of large system and complex control, etc., and achieve the effects of simple topology, improved reliability, improved integration and space efficiency

Active Publication Date: 2016-04-06
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, these methods mainly increase the reliability of the system by adding complex protection devices and special coordination control modules, which have the disadvantages of large system and complex control, and have not fundamentally solved the problem of traditional satellite power topology.

Method used

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  • Circuit topology and energy management method of satellite power source system
  • Circuit topology and energy management method of satellite power source system
  • Circuit topology and energy management method of satellite power source system

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Embodiment Construction

[0027] The present invention will be further introduced below in conjunction with the drawings.

[0028] Such as figure 1 As shown, the circuit topology of the satellite power supply system of the present invention includes a high-frequency transformer, m power modules, n energy storage modules, and k load modules. The high-frequency transformer is the core and the magnetic flux control of the high-frequency transformer is realized. The control requirements of each module. The high-frequency transformer has multiple primary and secondary sides, which are the hub connecting m power modules, n energy storage modules, and k load modules of different voltage levels and power levels. Therefore, the number of primary and secondary sides of the high-frequency transformer is m +n+k, where m, n, and k are all positive integers. The power module is located on the primary side of the transformer, and the energy storage module and the load module are located on the secondary side of the tr...

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PUM

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Abstract

The invention discloses a circuit topology and energy management method of a satellite power source system. The circuit topology comprises a high-frequency transformer, a plurality of power source modules, energy storage modules and load modules; the high-frequency transformer has a plurality of primary and auxiliary sides; and the power source modules, the energy storage modules and the load modules are connected with corresponding primary and secondary sides of the high-frequency transformer respectively through connecting terminals. According to the circuit topology of the invention, the high-frequency transformer is adopted, and therefore, the circuit topology is simple in circuit structure and control, has high power density and energy density, can simultaneously drive loads of different voltage levels and power levels load and can realize fault operation and coordinated control on power generation, energy storage and loads, and therefore, the circuit topology can be widely applied to high-frequency control systems such as a satellite power source system and a motor vehicle driving and energy management system.

Description

Technical field [0001] The present invention relates to the field of satellite power supply systems, in particular to a circuit topology and energy management method of a satellite power supply system. Background technique [0002] The satellite power system provides power supply for all the electrical equipment on the satellite. The reliability, stability and anti-interference ability of the satellite power system determines the operation status of the satellite and the realization of the satellite's complex functions. [0003] The traditional satellite power system connects multiple sets of solar panels in series and parallel, realizes centralized power supply through electronic power equipment such as PCU, and uses multiple secondary power supplies to convert the bus voltages of multiple sets of solar panels in series and parallel into each load. Grade voltage. The power supply system has a large number of power supplies, fault isolation, complex protection design, and cannot d...

Claims

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Application Information

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IPC IPC(8): H02S40/30H02J7/35
CPCH02J7/35H02S40/00Y02E10/50
Inventor 康庆邢杰焦荣惠李雅琳宋鼎邹仁炜李大伟关春键
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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